DocumentCode
943183
Title
A Reliability Analysis of Recoverable Missiles
Author
Broeder, George G den, Jr. ; Kane, William E.
Author_Institution
Lockheed Missile Systems Division, Palo Alto, California
fYear
1959
fDate
6/1/1959 12:00:00 AM
Firstpage
34
Lastpage
40
Abstract
-Missiles with built-in recoverability features have been of interest to most missile firms and many related firms for some time. In order to evaluate the adequacy of recoverable missile performance, it is frequently necessary to answer such questions as, ``With what probability will m such missiles yield a total of N or more successful flights?´´ or, ``How many missiles should be allocated to a test program in which N or more successful flights must be realized with probability Q?´´ Answers to these questions are obtained in terms of three basic reliability characteristics: 1. probability of a successful flight, 2. probability of recovering after a successful flight, and 3. probability of recovering after an unsuccessful flight. In addition, a decision rule is derived for selecting the ``best´´ reliability program.
Keywords
History; Missiles; Probability distribution; Testing; Tin; Vehicles;
fLanguage
English
Journal_Title
Reliability and Quality Control, IRE Transactions on
Publisher
ieee
ISSN
0097-4552
Type
jour
DOI
10.1109/IRE-PGRQC.1959.5007207
Filename
5007207
Link To Document